|
SAE AMS 2419 : 2015
|
PLATING, CADMIUM-TITANIUM |
|
SAE AS 1701 : 2017
|
LUBRICANT, SOLID FILM |
|
SAE AMS A 21180 : 2011
|
ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH |
|
MIL I 8500 : D
|
INTERCHANGEABILITY AND REPLACEABILITY OF COMPONENT PARTS FOR AEROSPACE VEHICLES |
|
SAE ARP 926 : 1997
|
FAULT/FAILURE ANALYSIS PROCEDURE |
|
FAA AC 23-13 : 2005
|
FATIGUE, FAIL-SAFE, AND DAMAGE TOLERANCE EVALUATION OF METALLIC STRUCTURE FOR NORMAL, UTILITY, ACROBATIC, AND COMMUTER CATEGORY AIRPLANES |
|
SAE AMS QQ C 320 : 2000
|
CHROMIUM PLATING (ELECTRODEPOSITED) |
|
MIL STD 130 : N
|
IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
|
TT P 1757 : B
|
PRIMER COATING, ALKYD BASE, ONE COMPONENT |
|
MIL STD 810 : G
|
ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
|
MIL STD 31000 : A
|
TECHNICAL DATA PACKAGES |
|
MIL HDBK 831 : A
|
PREPARATION OF TEST REPORTS |
|
SAE AMS A 22771 : 2012
|
ALUMINUM ALLOY FORGINGS, HEAT TREATED |
|
SAE AMS H 6088 : 2000
|
HEAT TREATMENT OF ALUMINUM ALLOYS |
|
MIL HDBK 275 : A
|
GUIDE FOR SELECTION OF LUBRICANTS, FLUIDS AND COMPOUNDS FOR USE IN FLIGHT VEHICLES AND COMPONENTS |
|
MIL STD 889 : C
|
DISSIMILAR METALS |
|
MIL STD 1537 : C
|
ELECTRICAL CONDUCTIVITY TEST FOR MEASUREMENT OF HEAT TREATMENT OF ALUMINUM ALLOYS, EDDY CURRENT METHOD |
|
SAE AS 9100D : 2016
|
QUALITY MANAGEMENT SYSTEMS - REQUIREMENTS FOR AVIATION, SPACE AND DEFENSE ORGANIZATIONS |
|
NASM 33540 : 2003
|
SAFETY WIRING, SAFETY CABLING, COTTER PINNING, GENERAL PRACTICES FOR |
|
SAE ARP 4761 : 1996
|
GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT |
|
SAE AS 5272 : 2016
|
LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING, PROCUREMENT SPECIFICATION |
|
SAE AMS S 13165 : 2007
|
SHOT PEENING OF METAL PARTS |
|
SAE AMS STD 2175 : 1998
|
CASTINGS, CLASSIFICATION AND INSPECTION OF |
|
MMPDS 07 : 2012
|
METALLIC MATERIALS PROPERTIES DEVELOPMENT AND STANDARDIZATION (MMPDS) - COMPLETE SET INCLUDES 9 CHAPTERS |
|
SAE AS 8879 : 2004
|
SCREW THREADS - UNJ PROFILE, INCH CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER |
|
MIL A 8625 : F
|
ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
|
ASTM E 1444 : 2005
|
Standard Practice for Magnetic Particle Testing |
|
ISO 10012:2003
|
Measurement management systems — Requirements for measurement processes and measuring equipment |
|
SAE AMS F 7190 : 2016
|
FORGING, STEEL, FOR AIRCRAFT/AEROSPACE EQUIPMENT AND SPECIAL ORDNANCE APPLICATIONS |
|
MIL HDBK 838 : 0
|
LUBRICATION OF MILITARY EQUIPMENT |
|
SAE ARP 4386 : 2010
|
TERMINOLOGY AND DEFINITIONS FOR AEROSPACE FLUID POWER, ACTUATION AND CONTROL TECHNOLOGIES |
|
SAE AMS C 8837 : 2015
|
COATING, CADMIUM (VACUUM DEPOSITED) |
|
SAE AMS C 26074 : 2013
|
ELECTROLESS NICKEL COATINGS |
|
SAE ARP 5311 : 2016
|
AEROSPACE-INTERFACE DEFINITION FOR MECHANICAL ACTUATION SUBSYSTEMS |
|
MIL PRF 46010 : H
|
LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING NATO CODE S-1738 |
|
FAA AC 25.613-1 : 2003
|
MATERIAL STRENGTH PROPERTIES AND MATERIAL DESIGN VALUES |